Spinning and related problems at high angles of attack for high-speed airplanes /
Walter J. Klinar.

Description

Main Author

Klinar, Walter J.

Related Names

Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1956.

Subjects

Charts, diagrams, etc.
Stalling (Aerodynamics)
Spin (Aerodynamics)
Airplanes > Airplanes / Control.
Fighter planes.
Supersonic planes.

Summary

A discussion is presented of the type of control manipulation and various techniques that may be required for satisfactory spin recovery of contemporary fighter designs. The effects in spins of jet-engine installations and the effectiveness of canard surfaces in alleviating a directional divergence near the stall and subsequent spin entry on one configuration are also discussed.

Note

NACA Research Memorandum L55L23A.
"March 19, 1956."
Title from cover.

Physical Description

8 p. : ill. ; 27 cm.

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